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A comparative study of elliptical and round scramjet combustors by Improved Delayed Detached Eddy Simulation 会议论文
21st AIAA International Space Planes and Hypersonics Technologies Conference, Xiamen, China, 6-9 March 2017
Authors:  Yao W(姚卫);  Yuan YM(袁越明);  Li XP(李晓鹏);  Wang J(王晶);  Fan XJ(范学军);  Fan, Xuejun(xfan@imech.ac.cn)
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Adiabatic Flame Temperature  Aerodynamics  Boundary Layer Flow  Boundary Layers  Chemical Analysis  Combustion  Computational Chemistry  Directed Graphs  Flow Separation  Mach Number  Principal Component Analysis  Regression Analysis  Sensitivity Analysis  Spacecraft  Supersonic Aerodynamics  Supersonic Aircraft  Transients  
Force Test in a Large-Scale Shock Tunnel 会议论文
55th AIAA Aerospace Sciences Meeting , Grapevine, Texas, 9-13 January 2017
Authors:  Wang YP(汪运鹏);  Liu YF(刘云峰);  Luo ZT(罗长童);  Jiang ZL(姜宗林)
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Detailed transitional process of the flames in hot and diluted environments from lifted flames to MILD combustion 会议论文
10th U.S. National Combustion Meeting, College Park, MD, United states, April 23, 2017 - April 26, 2017
Authors:  Liu CY;  Zhang J(张健)
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Oxygen  Diluted environments  Monotonic trend  Partial premixing  Stabilization mechanisms  Transition process  Transitional flames  Transitional process  Turbulent combustion  
INVESTIGATION OF OBSTACLE EFFECTS ON THE AERODYNAMIC PERFORMANCE OF FLAPPING WINGS 会议论文
ASME Fluids Engineering Division Summer Meeting, Waikoloa, HI, JUL 30-AUG 03, 2017
Authors:  Yin B(银波);  Yang GW(杨国伟);  Yin, B (reprint author), Chinese Acad Sci, Inst Mech, Key Lab Mech Fluid Solid Coupling Syst, Beijing, Peoples R China.
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Immersed-boundary Method  Micro-air Vehicles  Insect Flight  Vortices  Forces  Flows  
EXPERIMENTAL AND NUMERICAL STUDY OF THE CLOUD CAVITATING FLOW AROUND A SLENDER CYLINDER WITH A PETALS-SHAPED SECTION 会议论文
ASME Fluids Engineering Division Summer Meeting, Waikoloa, HI, JUL 30-AUG 03, 2017
Authors:  Wang YW(王一伟);  Huang J(黄荐);  Xu C(徐畅);  Yu C(余超);  Huang CG(黄晨光);  Wu XC(吴小翠);  Wang, YW (reprint author), Chinese Acad Sci, Inst Mech, Key Lab Mech Fluid Solid Coupling Syst, Beijing, Peoples R China.;  Wang, YW (reprint author), Univ Chinese Acad Sci, Sch Engn Sci, Beijing 100049, Peoples R China.
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Large-eddy Simulation  Hydrofoil  Propeller  Surface  
Normal acceleration reduce guidanceand control for sub-orbit vehicle re-entry 会议论文
21st AIAA International Space Planes and Hypersonics Technologies Conference, Xiamen, China, 6-9 March 2017
Authors:  Li WH(李文皓);  Xiao XX(肖歆昕);  Zhang H(张珩);  Xiao XX(肖歆昕)
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Aerodynamics  Air Navigation  Angle Of Attack  Control Surfaces  Control Theory  Degrees Of Freedom (Mechanics)  Dynamic Models  Flight Control Systems  Flight Simulators  Monte Carlo Methods  Reentry  Spacecraft  Surface Reactions  Uncertainty Analysis  Vehicles  
Effects of Shock Impingement on Aerothermal and Aerodynamic Performance for High-pressure Capturing Wings 会议论文
21st AIAA International Space Planes and Hypersonics Technologies Conference, Xiamen, China, 6-9 March 2017
Authors:  Li GL(李广利);  Cui K(崔凯);  Xiao Y(肖尧);  Xu YZ(徐应洲)
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Aerodynamics  Angle Of Attack  Angle Of Attack Indicators  Boundary Layers  Drag  Drag Coefficient  High Pressure Effects  Hypersonic Aerodynamics  Hypersonic Flow  Spacecraft  
Preliminary Study of Aerodynamic Performance for Waverider-based Hypersonic Vehicles with Dorsal Mounted Engines 会议论文
21st AIAA International Space Planes and Hypersonics Technologies Conference, Xiamen, China, 6-9 March 2017
Authors:  Xiao Y(肖尧);  Cui K(崔凯);  Li GL(李广利);  Xu YZ(徐应洲)
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Aerodynamics  Air Engines  Aspect Ratio  Computational Fluid Dynamics  Drag  Engines  Hypersonic Aerodynamics  Lift  Lift Drag Ratio  Propulsion  Spacecraft  Vehicles  
Study on Compression Surface Deformation of Waveriders 会议论文
21st AIAA International Space Planes and Hypersonics Technologies Conference, Xiamen, China, 6-9 March 2017
Authors:  Xu YZ(徐应洲);  Cui K(崔凯);  Li GL(李广利);  Xiao Y(肖尧)
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Aerodynamic Configurations  Aerodynamics  Computational Fluid Dynamics  Deformation  Evolutionary Algorithms  Fluid Dynamics  Hypersonic Aerodynamics  Optimization  Spacecraft